View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 68324U 26145.54917098 +.00000000 +00000-0 +73543-3 0 00002
2 68324 53.1584 351.2331 0001876 83.4445 276.6769 15.30196356 01
| Epoch (UTC): | 25 May 2026 13:10:48 |
| Eccentricity: | 0.0001876 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 351.2331° |
| argument of perigee: | 83.4445° |
| revolutions per day: | 15.30196356 |
| mean anomaly at epoch: | 276.6769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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